Control system



Dec. 26, 1944. J. N. GooD CONTROL SYSTEM original Filed July 3o, 1942 2 Sheets-Sheet l ly., Q5 l HIE gg 101 45 A N Mullin@ 52 7e 75 5o 51 97 5 6a ee; 67-66 6a um 51 75 56r z 'll'u 51 77 fff ni-.f my un fw "1m l 51 "'f. llu- 'f- 7849 g4 il 5o 656065 105 eo .56 7.

INVENTOR John N'. Good BY ATTORNEY Dec. 26, 1944. J, N; G0013 i 2,366,020

CONTROL SYSTEM Original Filed July 30.` 1942 2 Sheets-Sheet 2 "Eig. 6

INVENTOR John N Good BY Pd ATTORNEY Patented Dec. 26, 1944 CNTROL SYSTEM John N. Good, Wilmerding, Pa., assignor to The Westinghouse Air Brake Company, Wilmerding, Pa., a corporation of Pennsylvania Original application July 30, 1942, Serial No. 452,950. Divided and this application April 30, 1943. Serial No. 485.115

7 Claims. (Cl. 192-01) This invention relates to a control system for controlling the operation of a prime mover such as a Diesel engine, and is a division of my co;-

pending application, Serial No. 452,950, led July 30, 1942.

In certain ships a plurality of Diesel engines, operated either singly or in multiple, are employed for driving a propeller. These engines are of the reversible type for .either turning the propeller in one direction to move the ship forwardly or in the opposite direction for moving the ship in an astern direction. The speed or power output of the engines is varied in accordance with the amount of fuel supplied to the engines and a clutch is employed for connecting and disconnecting each engine to and from the propeller.

When all of the engines are operating to turn the propeller in the same direction, they may all' be connected to the propeller, if desired, for propelling the ship in the direction determined by the engines. At times, however, one or more engines operating to turn the propeller in one direction will be connected to the propeller while the other engine or engines will be operating in a direction which if connected to the propeller would cause the propeller to turn in the oppositel v direction and, as will be apparent, it would be undesirable to connect the `latter to the propeller under this condition since it might result in damage to the engines or parts of the transmission system between the engines and propeller.

One object of the invention is therefore the provision of means arranged to prevent engines running in directions which would cause a common means to be operated to turn in opposite directions from being connected at the same time` to said means.

Another object of the invention is the provision of means for preventing the engines being connected with the propeller when operating' at a speed above a certain low degree, such as idling.

Another object of the invention is the provision of a control system for a plurality of engines arranged to operate a common means, embodying I for each engine, a manual controller for controlv ling the starting of the engine in either one direction or the reverse direction, and for controlling a clutch for connecting and disconnecting the engine to and from said means, and also embodying means for preventing the operation of said clutch to connect said engine to said means when the engine is operating above aV chosen low speed or when the means is being operated by another engine operatingl above said chosen low speed, and further embodying means for preventing operation of said vcontroller to connect its engine running in one direction to said means when` said means 1s connected to another engine operating to turn said means in. the reverse direction.

Other objects and advantages will be apparent from the following more detailed description of the invention.

In the accompanying drawings; Fig. 1 is a diagrammatic View of a control system for a plurality of engines embodying the invention; Fig. 2 is a sectional view taken on the line 2--2 in Fig. l; Fig. 3 lis a sectional view taken on the line 3--3 in Fig. 2; Fig. 4 is a. sectional view taken on the line d-d in Fig. 2; and Figs..5 and 6 are views similar to Fig. 4 but with certain parts shown in'diierent positions,

Description In the drawings, the reference 'numerals I and 2 indicate two internal combustion engines which may be of the Diesel type, and both of which are arranged to be connected to operate a common propeller shaft 3 through the medium of suitable clutches 4 and 5, respectively, and a device t containinglsuitable gearing (not shown).

The clutches Il and 5 may be of any desired type arranged for operation by uid under pressure supplied thereto to connect the respective engine to the propeller shaft 3 and to disconnect said engine from the propeller shaft upon the release of such fluid under pressure.

Associated with engine I is a pneumatic starting control device 'I arranged to be conditioned by iiuid under pressure supplied through a pipe 8 to provide for operation of said engine in one direction and through a pipe 9 to provide for operation of said engine in the reverse direction.

A fuel supply device I0 is associated with engineI and embodies an adjustable member II for varying the fuel supply and thereby the speed or power output of said engine. For adjusting the member II it may be connected to one end of ,a lever I2 which is fulcrumed intermediate its ends. The opposite end of lever I2 may be con-l nected toa piston I3 contained in a cylinder I4 and subject on one sideto the pressure of a calibrated 'spring I5; At the opposite side of piston I3 is a pressure chamber I6 connected to a pipe I'I through which Iluidy under ypressure may be supplied .to andreleased from said chamber for adjustingthe 'position ofpiston I3 in cylinder Il andthereby the., position of the fuel governing member II in accordance with the `pres sure of such iiuid. With chamber I6 at 'sub-` stantially atmospheric/pressure spring l5 will urge the piston I3 to the position shown which may be assumed to be idling position to provide for operation of the engine at a chosen low or idling speed. When the piston I3 is moved in its cylinder by iluid pressure supplied to chamber I6 to a position, for instance, substantially midway of the length of the cylinder I4, it may be assumed that the fuel supply member will be positioned to provide for maximum speed or power output of the engine I. Intermediate positions of the piston 3, dependent upon the pressure of uid in chamber I6, will therefore provide corresponding intermediate degrees of speed or power output of engine I.

Associated with engine 2 is a pneumatic starting control device I3 like the device 1 but controlled by iiuid under pressure from pipes I9 and 20. The engine 2 has a fuel governing device 2| embodying a member 22 adjustable by a. lever 23 in accordance with the position of a piston 24 in a cylinder 25 as determined by the pressure of a spring 26 acting on one side of the piston and the opposing pressure of fluid supplied through a pipe 21 to a pressure chamber 28 to act on the opposite side of said piston. The piston 24 may have a position such as shown to provide for operation of the engine at idling speed and other positions depending upon the pressure of fluid in chamber 28 to provide corresponding speeds or degrees of power output as described in connection with piston I3 associated with engine I.

A manually adjustable control device 30 of any suitable type is provided for controlling the pressure of fluid in pressure chambers I6 and 23 and thereby the adjustment of pistons I3 and 24 and the speed or power output of engines I and 2, respectively. To accomplish this end the device 30 is connected to a pipe 3| which is arranged to be opened through cutoff valve devices 32 and 33 to pipes I1 and 2l leading to the pressure chambers I6 and 28, respectively. With the pressure chambers I6 and 26 thus connected to the control device 3D said device is operative to either open both of said chambers to the atmosphere to provide for operation of engines I and 2 at their idling speeds or to supply fluid at any desired pressure from a iluid pressure supply pipe 34 to both of said chambers to cause operation of said engines at a chosen higher speed or degree of power output.

The cutoi valve device 32 is provided to render the engine I non-responsive to an increase in uid pressure provided in pipe 3| by operation of control valve device 30, if it is desired that the engine I be disconnected from the propeller shaft 3 and be operating at idling speed, while the engine Z is operating said shaft to propel the craft at a` speed determined by operation of the control valve device 30. The cutoff valve device 33 is provided to accomplish the same result, with respect to engine 2.

Both of the cutoil valve devices 33 and 32 may be of the same construction, each comprising a double beat valve 35 having one position for opening communication between pipe 3| and the respective pipe I1 or 21 and another position for closing such communication and opening the latter pipe |1 or 21 to atmosphere. A spring 36 in each cutoif valve device is operative to move the double beat valve 35 to the position for connecting pipe 3| to pipe I1 or 21, while an electromagnet 31 is arranged for operation upon energization to move the double beat valve to its other position for closing communication between pipe 3| and pipe I1 or 21 and opening the latter to atmosphere.

The electromagnets 31 of the cutoff` valve'devices 32 and 33 are arranged to be energized by electric current frokm any suitable source such as a, battery sa. A ulanuauy operative switch 3s is provided in the circuit to magnet 31 of the cutoil valve device 32, while a corresponding switch 49 is provided in the circuit to the magnet of the cutoff valve device 33. Closing these switches is arranged to effect energization of the respective electro-magnets while opening the switches is arranged to effect deenergization of said magnets. With the magnets deenergized, it will therefore be seen that the engines and 2 will operate in accordance with operation of the manual control device 30, and that with the magnets energized the engines will be non-responsive to operation of the control device 30 and will operate only at idling speed. These switches and the cutoff valve devices 32 and 33 are therefore effective to cut out either one engine or the other, as desired.

According to the invention I provide a manual control device 45 for controlling the starting control device 1 and the clutch 4 for engine I. This manual control device also embodies means controlled from pipe 3| for preventing operation of clutch 4 to connect engine I to the propeller shaft 3 with either engine operating above a chosen low speed, such as idling. A similar manual control device 4'6 is provided for controlling the starting control device I8 and clutch 5 for engine 2 and is also provided with means controlled from the speed control pipe 3| for preventing engagement of clutch 5 with either engine operating above a chosen low speed, such as idling. Means are also provided for preventing operation of both of the manual control devices 45 and 46 to connect both engines and 2 to the propeller at the same time when the engines are operating in directions which would cause the propeller to turn in opposite directions.

The control device 45 comprises a casing having two spaced aligned bearings 49 and 50 in which a rock shaft 5| is journaled. A cage 52 interposed between and bearing against the adjacent ends of bearings 49 and 50 has aligned openings through which the shaft 5| extends. Between the l'bearings 49 and 5D the shaft 5| has a slot 53 extending diametrically therethrough and the cage 52 has an aligned slot 54. An operating member 55 of substantial disk form is disposed in slot 53 and extends into slot 54 and is journaled at its axis on a pin 56. The pin 56 is arranged at right angles to the axis of shaft 5| and is carried in suitable vbores in said shaft at opposite sides of slot 53 and in the adjacent portions of :cage 52. The thickness of the operating' member 55 is less than the width of slots 53 and 54 only sufficiently to provide free rocking move ment about the pin 56. The cage 52 being secured to shaft 5| by pin 56 holds the rock shaft 5| against endwise movement.

The operating member 55 is formed on one end of a lever 51 and from the above description it will be seen that the pin 56 provides for rocking of said lever and member on said pin relative to the rock shaft 5I in the direction of the length oi said shaft, while said rock shaft provides for movement of said lever and operating member at right angles to the axis of the shaft, the operating member 55 under this latter condition providing an operating connection between said lever and shaft for turning the shaft with the lever.

A starting control valve device 82 is provided in the casing at one side of rock shaft :beyond the adjacent end oi' pin 56. .This device comprises a vertically movable plunger 83 (Fig. 3) and valve `means (not shown) operable upon downward movement of said plungerv to supply Afluid under pressure from the supply pipe 34 to the starter control -pipe 9 for actuating the starter control device 1 to provide for starting'of the engine in one direction It may be assumed that, with the engine I operating in this direction the propeller shaft 3 when connected to said engine will cause movement of the ship in a forwardly direction. Movement of the plunger 83 in an upwardly di-r rection as viewed in Fig. 3 is arranged to allow release of iluid under pressure from the starter control pipe 8 to provide for stopping of the engine or for starting of the engine in the opposite direction, as will be later described.

For controlling the plunger '83 one end of a lever 64 bears against the plunger. This lever is supported on a pin 85 secured in the casing While the opposite end is provided with a roller 86 arranged lto contact a cam surface 81 provided on the cage 52 above one end of pin 56 and adjacent the top of operating member 55; Movement ofv the member 51 toward the left-hand as seen in Fig. 3 or upwardly as viewed in Fig. 1, to a position bearing the legend Forward is arranged to -operate cam 81 and thereby the lever 64 to move the plunger 83 in a downwardly direction for supplying iluid under pressure to the starter control pipe 9, while movement of said vlever back to its normal position shown is arranged to provide for movement of the plunger83 in the reverse direction for releasing fluid under pressure from pipe 6.

At the opposite side of shaft 5| and beyond the opposite end of pin 56 is a starting control valve device 88 which may be identical to the device 82 and which comprises a plunger 89 operable upon downward movement to supply fluid under pressure from the supply pipe 34 to pipe 8 leading to the starter control device to provide for operating of said device to cause starting of ,the engine l in the direction of the reverse of that attained by the supply of fluid under pressure to pipe 8, or in a direction to cause movement of the ship in an astern direction when connected to the propeller shaft 3, as indicated by the legend Astern in'Figs. l and 3.

A lever 98 like lever 84 is arranged for controlling movement of'plunger 89, and the cage 52 is provided with a cam 8| opposite the cam 81 for operating the lever 90. By this construction movement of the operating lever 51 downwardly is viewed in Fig. 1 or in the direction of the righthand, as viewed in Fig. 3, will actuate the valve device 68 to cause starting of the engine in the direction to provide for astern movement of the ship, while return of the lever 51 to the neutral 'position shown will provide for operation of the valve device 88 to release fluid under pressure from pipe 8 in order to eiect stopping or reversal l of the engine.

l slot 92 extending at right angles to the axis oirock shaft 5|. This slot provides for movement of the vlever 51- to either "Forward position or Astem position for actuating the starter control valve devices 82 and 88 respectively for starting the engine I in either one direction or in the reverse direction as above described, and to the neutral position for stopping the engine. vIt will be seen that this slot prevents movement of the lever 51 in any directionexcept for operating the valve devices 82 or 88. Y

A clutch control device 68 is associated with the casing bearing 50 beyond the journaled end of shaft 5|. This device comprises two oppositely seating poppet valves 6| and 62 ,arranged in coaxial relation with rock shaft 5| and contained in chambers 63 and 64, respectively. These valves have iluted stems extending toward each other through suitable bores in the device and meeting in a chamber 65. The chamber 63 is connected by a pipe 66 to the uid pressure supply pipe 34 and .contains a spring 61 acting lon the valve 6| for seating same and at the same time unseating the valve 62. The chamber 65 is connected by a pipe 68 to the clutch 4 for engine The chamber 64 is open through a passage 69 to the interior of the casing and thus with the atmosphere through openings including slot 92.

The rock shaft 5| between the operating member 55 and valve 62 is provided with an axial bore in which is slidably mounted a plunger 10. One end of this plunger engages the valve 62 while the other end is aligned for engagement by the peripheral surface of the operating member 55 at one side of pin 56. The operating member 55 has in its peripheral surface a recess 1| arranged to receive the adjacent end of plunger 10 when the operating lever 51 is in the vertical position shown in Figs. 1 and 2. With the plunger 16 in recess 1| spring 61 is operative to seat valve 6| and open valve 62 to thereby connect the clutch control pipe 58 to the atmosphere for effecting operation of the clutch 4 to disconnect the engine from the propeller shaft. Movement of the lever 51 from this vertical position in either a clockwise direction or counterclockwise direction, as viewed in Fig. 2, is adapted toturnv the operating member 55 to a position in which a portion at either one side or the other of recess 1| is in engagement with the plunger 18 and during such movement eiect movement of the plunger 16 outwardly of shaft 5| to seat valve 62 and unseat valve 6|. With the valve 6| thus open fluid under pressure will flow from the supply pipe 34 to pipe 68 and thence to clutch 4 for eecting operation thereof to connect the engine to the propeller shaft 3.

In order that the lever '51 may be operated as just described for controlling the operation of the clutch 6, the top wall 9| of the casing is pro-v vided with two oppositely extending slots 93 and 94 opening to the opposite sides of the slot 92 adjacent its opposite ends. It will be seen that since engagement of the clutch 4 is dependent upon movement of the lever 51 in either a clockwise or counterclockwise direction from the position shown in Fig. 2 and thus out of the slot 92, the clutch will be disengaged-with the lever in the slot 92 and be engaged only upon movement into the slot 93 or into the slot 84.

In use, let it be assumed that the lever 51 is in its neutral position midway between the ends of slot 92 as shown in Figs. 1 and 3. If it is now desired to start the engine in such a direction as to cause operation of the propeller shaft 3 to move the ship forwardly the lever 51 is moved in slot 92 to Forward position for thereby operata ing the starter control valve'device 82 to cause the engine to be started in a direction to obtain forward movement of the ship. After the engine is thus started, the lever 51 is drawn back from the end of slot 92 to a position aligned with slot 93 and then moved into the latter slot for operating the clutch control device 80 to supply iluid under pressure to pipe 88 for actuating the clutch 4 to connect the engine I to the propeller shaft 3, whereupon the engine will operate the propeller of the ship to cause movement of same in a forwardly direction.

On the other hand, if it is desired that the ship move in an astern. direction, the lever 51 is moved either from its neutral position, or from Forward position through its neutral position which causes stopping of the engine, to its Astern position at the opposite end of slot 92 to thereby actuate the starter control valve device 88 to supply fluid under pressure to pipe 8 for causing the engine I to be started in the reverse direction. The lever 51 may be then moved away from the end of slot 92 into alignment with slot 94 and then into the latter slot for actuating the .clutch control device 80 to supply fluid under pressure to pipe 68 for operating the clutch 4 to connect the engine to the propeller shaft 3 for causing movement of the ship in an astern direction.

It will be seen that with lever 51 in slot 92 the clutch control pipe 68 will be opened to atmosphere by way of the clutch control device 60 to effect operation of the clutch 4 to disconnect the engine I from the propeller shaft 3. Connecting the engine to the propeller shaft is obtained only upon movement of the lever into either slot 93 or slot 94. The slot 92 provides for starting of the engine in either one direction or the reverse direction before actuating the clutch 4 for connecting the engine to the propeller shaft and also ensures disconnecting the engine from the propeller shaft before reversing the engine.

Within the housing a spring seat 96 mounted on lever 51 rests on a shoulder 91 provided on the lever in substantial alignment with the upper end of cage 52. A friction shoe is slidably mounted on lever 51 between the spring seat 96 and inner surface 98 of the top wall of the casing. A coil spring 99 under pressure encircles the lever 51 and is supported at one end on the spring seat 96 and bears at the opposite end against the friction shoe |00 for constantly urging said shoe against the inner surface 98 of the casing.

The inner surface 98 is substantially in the shape of an inverted V in the direction of the length of slot 92 and in said surface adjacent each of the opposite ends of said slot is a recess I0| arranged to receive the shoe |00 upon movement of the lever into alignment with either of the slots 93 or 94. With the shoe |00 engaging the surface 98 at any point between the two recesses I0| the. force of the spring 99 againstsaid shoe is operative to automatically return the lever 51 to its neutral position shown in Fig. 3. When the shoe |00 is in either of the recesses |0I, the lever 51 is held against movement toward neutral position. By this arrangement it is necessary for the operator to move the lever 51 substantially to either one end or the other of slot 92 in order that the,lever will not return to its neutral position shown upon removal of manualy force on the lever. lever to cause starting of the engine in either one direction or the opposite, as desired, and also provides for the lever being held in its clutch engaging positions in slots 93 or 94 due to interlocking of the friction shoe |00 within the recesses |0|, and also due to the fact that the surface 88 This insures adequate movement of the lengthwise of these recesses is arranged at substantial right angles to the normal or neutral position of lever 51 in slot 92.`

A clutch and speed interlock device 15 is secured to the casing over the opposite end of rock vshaft 5|. This device. comprises a piston. 16 having at one side a chamber 11 open to the speed or powerv output control pipe 3|. Projectingfrom the opposite face of piston 16 is a plunger 18 which slidably extends through a suitable axial bore in the adjacent end of shaft 5| into alignment with the peripheral surface of the operating member 55 directly opposite that engaged by the plunger 10. 'I'he operating member 55 has a notch or recess 19 provided in its periphery in such a position as to receive the end of plunger 18 when the lever 51 is in slot 92 in which the clutch 4 disconnects the engine from the propeller shaft. A coil spring encircling the plunger 18 bears at one end against the adjacent end of rock shaft 5| and the opposite end bears against piston 15 in opposition to pressure of iluid effective in chamber 11.

As above described, the speed or output of engine is varied according to the pressure of fluid supplied to act in pipe 3|, and opening of said pipe to atmosphere provides for idling operation of said engine. The pressure of spring 80 on piston 16 in the interlock device 15 is such as to move said piston and plunger 18 to the position shown when the pressure in pipe 3| and thereby chamber 11 is at a chosen low degree, or substantially that of the atmosphere if desired, and to permit the piston to move the plunger 18 against the operating member 55 when the pressure in said pipe is increased above that degree. Thus if engine I should be operating at a speed above the chosen low degree with the lever 51 in slot 92, the plunger 18 will enter recess 19 and prevent turning of member 55 and thus maintain the clutch 4 in the position disengaging engine I from the propeller shaft 3. To rock the lever 51 in either direction from the clutch disengaging position shown in Fig. 2 to cause operation of clutch 4 to connect engine to the propeller shaft 3, the pressure in the speed control pipe 3| and piston chamber 11 on the interlock piston 16 must therefore be reduced to a degree which provides for operation of the engine at the chosen reduced speed. When this occurs, spring 80 will move the piston 16 and plunger 18 to the position shown in Fig. 2 in which the plunger 18 is removed from notch 19. When this condition exists, the lever 51 may be moved into either of the slots 93 or 94 for actuating the clutch 4 to connect the engine to the propeller shaft 3. In otherl words, the interlock valve device 15 controlled from the speed control pipe 3| prevents the operator moving lever 51 into either of the' slots 93 or 94 for actuating the clutch 4 to connect the engine I to the propeller shaft 3 when the engine is operating at a speed above a chosen low degree.

The manual control device 48 may be identical to the manual control device 45 and like reference numerals have therefore been applied to the main corresponding portions of the control device 48. In Fig. 2 it will be seen that the clutch control device 60, interlock valve device 15, and operating member 55 are disposed in the control device 46 just the reverse of corresponding parts in the control device 45 but this in no Way changes the operation of the engine 2 as controlled by the starting control device I8 or of clutch I5 in response to operation of lever 51 in the control device 4s in sion s2, es, and s4 which are identical to cdrresponding slots providing for controlling movement of lever -51 in the control device 45. The operator may, therefore, move lever 51 of the control device 46 upwardly in slot 92, as viewed in Fig. 1, to Forward position for causing starting of the engine 2 in adirection to propel the ship forwardly and then into the slot 92 for actuating clutch 5 to connect the engine to the propeller shaft 3, or he may move'said lever to the opposite end of slot 92 to Astern position for causing starting of the engine 2 in a. direction for moving the ship in an astern direction and then move said lever into slot 94 for actuating the clutch 5 to connect said engine to the propeller shaft 3, these operations being the same as in the control device 45 and producing the same results with respect to engine 2. Moreover, movement of lever 51 of the control device 46 to actuate clutch 5 to connect engine 2 to the propeller is subject to control by the respective interlock device 15 the same as above described in connection with the control device 45.

If the operator desires to connect both engines i and 2 to the propeller shaft 3 at the same time for driving the ship, he may move both levers 51 in the same direction to either one end or the opposite end of slots 92 and then into either slots 93 or 94, respectively, as will be apparent.

However, if one engine is already connected to the propeller shaft at the time it is desired to connect'the other engine to said shaft, the interlock device 15 of the controller 45 or 46 controlling the latter engine requires that the pressure in the speed control pipe 3| be such as to provide for idling operation not only of the respective engine, as above described, but also of 'the other engine and thereby ofthe propeller shaft 3, since said interlock device is controlled by the same pressure as controls the speed of the other engine. The interlock valve device thus precludes the possibility of connecting either engine to the propeller shaft when said shaft is being driven by the other engine `operating at a speed above idling. l

If one engine were operating in a direction to cause movement of the craft, say forwardly, it

would be undesirable to be able to connect the other engine operating in the reverse direction with the propeller shaft 3 at the same time, for reasons before pointed out. This however is prevented by a link |05 having one end pivotally connected with a pin |06 depending from the operating member 55 in the control device 45. The opposite end of link |05 has a slot |01 in which is disposed a pin |08 like the pin |06 but depending from the operating member 55 of the control device 46.

InFigs. 4, 5 and 6 the link |01 and the pins |06 and |08 are shown with the two levers 51 and the slots 92, 93 and 94 of the two control devices 45 and 46 superimposed therein in dot and dash form in order to clearly bring out the function of said link and pins.

With the two levers 51 midway between the ends of the respective slots 92 as shown in Fig. 4, it will be seen-that the pin |08 associated with the control device 46 is disposed intermediate the ends of slot |01 in the link |05 so that either of the levers 51 may be moved to either one end or the other of the respective slots 92 without interference from the link |05. l

Let it be assumed however that in the control peller shaft for causing movement of the ship in an asterndirection. as above described. Under this condition, the pin |05 in the control device 45 will occupy a position such as shown in Fig. 5 and its connection with pin |08 will prevent movement oi' lever 51 in the control device 46 into its slot 99 since the latter pin |08 is in engagement or substantially so with the end of slot |01 -in the link. It will, however, be seen that Y with the lever 51 of the control valve device 45 v,in slot 94, the lever 51 in control device 46 may be moved to the opposite end o! the slot 92 therein for starting the engine in the reverse direction, if such is desired.

If lever 51 in the control device 45 should be disposed in its slot 93 the operator could move the lever 51 in the control device 46 to the opposite end of its slot 92 for starting of the engine 2 under which 'condition the link 05 will assume an angular position the reverse of that shown in Fig. 5 for preventing movement of lever 51 in the control device d5 into its slot 94. On the vother hand, if lever 51 in the control device 46 should be in its slot 95 as seen in Fig. 6, the inner end of slot |01 in link |05 will substantially engage the pin |59 and prevent movement of the lever 51 in the control device 55 into slot 53. In case the lever 51 in the control device 55 should be in slot 93 and the lever 51 oi the control device 55 should be moved to the opposite end of its slot 92, the link |05 will assume a position the reverse of that shown in Fig. 6 and prevent movement of the latter lever 51 into its slot 94. The link |05 thus provides for intended operation of the control devices 45 or 46 either singly or jointly but prevents undesired operation thereof.

Summary It will now be seen that have provided an arrangement whereby a plurality of reversible internal combustion engines operating to cause movement of 'a driven member in a certain direction may be connected either singly or collectively by individual manual control devices to operate said driven member. These control devices also control the direction which the engines are started and operate and thus the direction which the driven member will move when connected to the engines. A simple mechanical interlock is provided between the control devices to prevent connecting the driven member to an engine which is operating in aone direction when the driven member is already connected to another engine operating in the reverse direction. Moreover, the arrangement embodies means for preventing the operation of a clutch to connect an engine to the driven member when that engine or another engine connected to the driven member is operating at a speed above a certain low speed, so as to thereby avoid damage to the clutch, engine, or other parts of the power system.

Having now described my invention, what I claim as new and desire to secure by Letters Patent, is:

1. A system for controlling the power output of an internal combustion engine and the connecting and disconnecting of said engine to and from a member to be driven, said system comprising in combination, power control means adjustable to vary the power output of said engine and having a condition providing for operation offsaid. engine at a chosen reduced output, manually operable means for adjusting said power control means. coupling means for connecting and di'sconnecting said engine to and from said member, a manually operable lever for controlling said coupling means and having one position to effect operation oi' said coupling means 'for disconnecting said engine from said member and movable to another position to effect operation of said coupling means to connect said engine to said member, and means controlled by said manually operable means operable to prevent movement of said lever from said one position with said power control means adjusted to provide an output of said engine substantiallyabove said chosen reduced output.

2. A system for controlling the power outputl of an internal combustion engine andthe connecting and disconnecting of said engine to and from a member to be driven comprising in combination, power control means adjustable by uid under pressure to vary the power output of said engine in accordance with the degree of such pressure, manually operable means for varying the pressure of fluid on said control means from a chosen low degree providing for operation of said engine at a chosen reduced output through a range to a higher degree to provide for corresponding increased output of said engine, a manually operable lever separate from said manually operable means having one position for disconnecting said engine from said member and another position for connecting said engine to operate said member, and means controlled by the pressure of fluid controlling said power control means and operable to prevent movement of said lever from said one position when the pressure of fluid is above said chosen low degree and providing for movement of said lever from said one position to said other position when the pressure of fluid on said power control means is at or below said chosen degree.

3. .A system for controlling the power output of an internal combustion engine and the operation of a clutch to connect and disconnect said engine to and from a member to be driven comprising in combination, power control means adjustable by fluid under pressure to vary the power output of said engine in accordance with the degree of such pressure and to provide a chosen reduced output when such pressure is at a chosen low degree, manually operable means for varying the pressure of fluid on said power control means, a manually operable lever separate from said manually operable means, valve means operable upon movement of said lever from a certain position for eiecting operation of said clutch to connect said engine to said member and upon return to said certain position to eilect operation of said clutch to disconnect said engine and member, a movable abutment subject to pressure of iluid on said power control means and operative when such pressure exceeds said low degree and with said lever in said certain position to secure said lever against movement, and means acting on said abutment for actuating same to release said lever for movement when the pressure on said power control means is at substantially said chosen reduced degree.

4. A system for controlling the power output of an internal combustion engine and the connecting and disconnecting of said engine to and from a member to be driven comprising in combination, power control means adjustable by fluid under pressure to vary the power output of said engine in accordance with the degree of such pressure and operative to provide a chosen reduced output when said pressure is of a chosen low degree, manually operative means operable to adjust the pressure oi.' fluid on said power control means, valve means for controlling said clutch, a manually operable lever for controlling said valve means having a certain position for effecting operation of said valve vmeans for actuating said clutch to disconnect said engine from said member and being operable upon movement to another position for actuating said valve means to effect operation oi.' said clutch to connect said engine and member, said manually operative means being operable independently of said lever, and means controlled by pressure of fluid on said power control means and cooperative with said lever in said certain position for securing same against movement when the pressure of iiuid on said power control means exceeds said chosen low degree and releasable from said lever to provide for movement thereof when the pressure on said power control means is substantially at said chosen low degree.

5. A system for controlling the starting of an internal combustion engine the operation of a clutch to connect said engine to a member to be driven and for also controlling the power output of said engine comprising in combination, power control means adjustable to vary the power output of said engine and conditionable to provide for operation of said engine at a chosen reduced output, a lever having a first position for stopping said engine, a second position for starting said engine and being operative in both of said positions to effect operation of said clutch to disconnect said engine from said member, said lever being movable to a third position to eil'ect operation of said clutch to connect said engine to said member, and interlock means operable in accordance with operation of said power control means to provide for movement of said lever to said third position with said control means adjusted to provide for operation of said engine at said chosen reduced output and to prevent operation of said lever to said third position with said power control means adjusted to provide a greater engine output, said interlock means providing for movement of said lever to said rst and second positions regardless of adjustment of said power control means.

6. A system for controlling the direction of starting of an internal combustion, the power output of said engine, and the operation of a clutch to connect and disconnect said engine to and from a member to be driven, said system comprising in combination, power control means adjustable by iluid under pressure to vary the power output of said engine in accordance with the degree of such pressure and to provide for operation oi.' said engine at a chosen reduced output when said pressure is of a chosen reduced degree, manual control means operable to vary the pressure of iiuid on said power control means, a lever having a position for stopping said engine and for effecting operation of said clutch to disconnect said engine from said member, and being movable in a certain direction from such position to effect starting of said engine in one direction and in the opposite direction from said certain position to effect starting of said engine in the reverse direction, said lever being also operable upon movement in a different direction to actuate said clutch to connect said engine to said member, and interlock means subject to pressure of fluid in said power control means and cooperative with said lever, in its plane of movement for controlling the stopping and starting oi' said en-l gine, to secure same against movement inthe direction for effecting operation of said clutch to connect said engine to said member when the pressure of fluid in said power control means is above said chosen reduced degree, and providing for operation of said lever to eiect operation of said clutch to connect said engine and member when the pressure of fluid in said power control means is at or below said chosen degree.

7. A device for controlling the direction of operation of a reversible internal combustion'engine having means controlled by fluid pressure for varying the power output of said engine in accordance with the pressure of such fluid and which provides for operation of said engine at a chosen reduced output when such pressure is at a chosen reduced degree, said device being also operative to control the connecting and disconnecting of said engine to and from a member to be driven and for preventing said engine being second position to eiect koperation of said valve means for causing starting of said engine in one direction and being also movable in said plane in the opposite direction from neutral position to a thirdy position for effecting operationof said valve means to cause starting of said engine in the reverse direction, said lever in said plane providing for operation of said valve device and thereby of said clutch toA disconnect said engine from said member, said lever being movable out of said plane adjacent either said second or third positions for actuating said valve device to effect operation of said clutch to connect said engine to said member, a spring, and a movable abutment subject to the opposing pressures of' said spring and of iluid pressure controlling the output of said engine, said abutmentbeing movable by said iiuid pressure when above the degree which provides said chosen reduced output, into contact with said lever and said spring being operable to move said abutment out of contact with said lever when the pressure of fluid is at or below said reduced degree, and means associated with said lever arranged to interlock with said abutment when said lever is in said plane to prevent movement of said lever out of said plane but providing for movement o1 said lever in said plane. f

' JOHN N. GOOD. 

